137 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 137 total) Small, Inflatable, High Pressure Composite Tanks for Human Spaceflight One of the issues facing the development of manned, long duration space missions is how to manage liquids/gases for life support. Gases such as O2, CO2, CH4 etc are inputs and by-products of life support systems, for non-regenerative (open-loop) systems. Stores should be enough to sustain any short duration crew visit and until regenerating (closed loop) systems can be installed. Italy TDE T324-502QT THALES ALENIA SPACE ITALIA SPA 2018 - 2021 Small, Inflatable, High Pressure Composite Tanks for Human Spaceflight Hypersonic simulation tool based on Lattice Boltzmann solver Over the last few years schemes based on minimal kinetic models for the Boltzmann equation are becoming increasingly popular as a reliable alternative over conventional Computational Fluid Dynamics (CFD) techniques. Due to the flexibility afforded by its close connection to the kinetic theory recent research has led to major improvements, including consistent models for aerothermodynamics and highly compressible flow in low gravity operating conditions. Belgium TDE T718-505MP CENAERO. CENTRE DE RECHERCHE EN AERONAUTIQUE ASBL 2018 - 2021 Hypersonic simulation tool based on Lattice Boltzmann solver Powder Metallurgy Based Materials for High Wear Resistance, High Hardness and High Temperature This activity will consist of identifying and possibly modifying (composition, process parameters) powder metallurgy materials used in other industries with similar requirements (e.g. aeronautics, medical industry) or promising novel/advanced materials. United Kingdom GSTP G61A-006QT TWI LIMITED - THE WELDING INSTITUTE 2018 - 2021 Powder Metallurgy Based Materials for High Wear Resistance, High Hardness and High Temperature Novel structural components for launchers/satellites applications using additive manufacturing technologies Additive manufacturing technologies are emerging as a process to machining for small series, complex and costly parts allowing reduction in cost and time. The combination of issues (fabrication of unique products, short series, need for weight reduction through topology optimization) makes AM processes attractive for developing a large family of metallic parts for launcher and satellite applications. Space-flight hardware design involves complex geometries that can be produced by AM. Spain GSTP GT1A-004MS FUNDACI?N ANDALUZA PARA EL DESARROL AEROESPACIAL 2018 - 2021 Novel structural components for launchers/satellites applications using additive manufacturing technologies Redesign of the ESA Deep Space Antennas feed system to support future Moon missions New L2 missions like Euclid and Plato will require high data rate reception in K-Band downlink (26 GHz). A new X/K-Band coaxial feed system was developed in a previous TRP activity and it will be deployed in the next years in DSA2 (Cebreros, Spain) and DSA3 (Malargue, Argentina). This feed system architecture will be considered the starting point for the re-design of a new feed system that will allow simultaneous uplink (22 GHz) and downlink (26 GHz).It is intended to trade-off at least two alternative feed system architectures and to perform the detailed design of the selected one. Spain TDE T312-501GS TTI 2018 - 2021 Redesign of the ESA Deep Space Antennas feed system to support future Moon missions Utilisation of the Proton Irradiation Facility at PSI for Component Radiation Studies This activity concerns execution of regular irradiation test campaigns on EEE components for flight on ESA and European space missions. Up to 240 hours per year of beam time is available free of charge on a priority basis for ESA. Additionally, a minimum of 500 hours per year is available for ESA sub-contractors, research institutes and other interested users at preferential hourly rates. The agency provides the facility with a detailed work programme of the test campaigns. Switzerland TDE T723-F07QE PAUL SCHERRER INSTITUT (PSI) 2018 - 2021 Utilisation of the Proton Irradiation Facility at PSI for Component Radiation Studies Advanced glass cell technology for extended GNSS atomic clocks lifetime Glass cells are typically used in Frequency Standard, both as reference cell, in the lamps for atomic pumping and as dissociator bulbs.When used in a lamp (RAFS or Mercury ion trap), the cell must be sufficiently resilient for avoiding limitations in the lifetime due to diffusion of material (i.e. Rubidium or Mercury) inside the bulb walls, given the combination of dissociation mechanisms and high temperatures. Switzerland TDE T606-502ET OROLIA SWITZERLAND SA 2018 - 2021 Advanced glass cell technology for extended GNSS atomic clocks lifetime Trade-off for very large space telescope mirrors Currently the size limit for primary mirrors of large telescopes is - due to the available Ariane-5 fairing - typically at 3.5m (Herschel). Future science (and most likely also Earth observation missions) will call for larger telescope sizes due to more demanding requirements on the light collecting efficiency and angular resolution. France TDE T716-403MM AIRBUS DEFENCE AND SPACE SAS 2018 - 2021 Trade-off for very large space telescope mirrors Quality Control Metadata Management System for Land Monitoring Services There is a specific requirement on the new land services focusing on continuous change monitoring. The current operational methods of land cover change detection are based on bi-temporal analysis for two points in time. These approaches are applied to 3 to 6 years mapping campaigns, while land cover changes occur continually. ;With this 3 to 6 year gap between inventories, all land change processes occurring in between are not captured. Full-fledged Land Cover Continuous Monitoring system of the land evolution is provided for EEA. Belgium GSTP G611-047EO SPACEBEL SA. 2018 - 2021 Quality Control Metadata Management System for Land Monitoring Services Investigating spectroscopy and forward model improvements for atmospheric retrieval of methane in the thermal infrared The aim of this study was to explore and consolidate the possible sources of methane (CH4) biases in retrievals from thermal infrared (TIR) sensors, to establish necessary actions and perform the related work for mitigating biases. The study distinguisged three types of error sources: spectroscopic knowledge and input data to radiative transfer models (RTM), forward model errors, and instrument biases. For achieving this goal, the study addresses three main objectives, corresponding to three identified tasks: France Discovery 15/029 SPASCIA 2018 - 2021 Investigating spectroscopy and forward model improvements for atmospheric retrieval of methane in the thermal infrared Pagination « First First page ‹‹ Previous page … 2 3 4 5 6 7 8 9 10 … ›› Next page Last » Last page Filter by Programme GSTP (63) TDE (52) Discovery (20) Preparation (2) Filter by Start Year (-) 2018 (137) Filter by End Year 2020 (30) 2021 (28) 2019 (27) 2023 (24) 2022 (14) 2024 (8) 2018 (6) Filter by Keywords ISRU (7) Moon (7) 38-Advanced Manufacturing (6) 4-Users (4) 32-Clean Space (3) 35-Technologies Enabling Breakthroughs in Science (3) Exploration (3) Lunar Lander (3) 2-Ground segment and operations (2) 2-Optical Payloads (2) 2-Space Segment - Platform (2) 3-Habitation (2) 3-Space Segment - Payload (2) 5-Space System Control (2) 9-Opportunity (2) 46-HERA (2) Optics (2) Remote Sensing (2) 0-Navigation Technologies (1) 0-Telecommunications Technologies (1) 1-Microwave Payloads (1) 1-Onboard Data Systems (1) 1-Phootprint (1) 1-Space Situational Awareness (1) 1-Systems (1) 2-Space Segment (1) 2-Space System Software (1) 3d printing (1) 4-Ground Segment (1) 4-Spacecraft Environment & Effects (1) 6-RF Systems, Payloads and Technologies (1) 7-Electromagnetic Technologies and Techniques (1) 8-System Design & Verification (1) 10-Flight Dynamics and GNSS (1) 11-Space Debris (1) 18-Aerothermodynamics (1) 20-Structures (1) 21-Thermal (1) 28-Electronic Components (1) 99-Others (1) active optics (1) Additive Manufacturing (1) Arctic Weather (1) Ariadna (1) Asteroids (1) Astronaut (1) Astronomy (1) Autonomy (1) basalt (1) Battery (1) Biology (1) Blue Economy (1) Boom (1) Carbon Fiber (1) CDF (1) CFRFE (1) Code (1) concurrent engineering (1) Constellation (1) DART (1) Developments (1) Doh (1) Doherty Power Amplifier (1) Earth observation (1) Energy Storage (1) EO (1) FCI (1) flexible coating (1) flexible OSR (1) geopolymer (1) GNSS (1) HAPS (1) HERA (1) Impact (1) Instrument (1) iSALE (1) ITI (1) Ka-band (1) Latch Valve (1) Li-Ion (1) lunar base (1) Lunar Surface (1) Manufacturing (1) Mars (1) Materials (1) mechanisms (1) Methane (1) MTG (1) Navigation (1) Ocean (1) optimal control (1) OSR (1) Power (1) power generation (1) Propulsion (1) Pseudo Satellites (1) quadrocopters (1) radiator (1) Regolith (1) reinforced (1) Safety (1) Satellite (1) shock physics (1) Simulation (1) smart OSR (1) SPH (1) Super resolution (1) Telecommunication (1) Telescope (1) TIR (1) topological optimization (1) X-ray (1) Filter by Contractor OHB System AG (5) GMV AEROSPACE AND DEFENCE, SA (3) Thales Alenia Space (3) ACONDICIONAMIENTO TARRASENSE ASSOCI (2) AIRBUS DEFENCE AND SPACE SAS (2) ATOS CONVERGENCE CREATORS GMBH (2) CSEM SA. 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